23-Aug-2011. 2. AFM. Revision 3. 0, 1. 9-A33-03,. 9-A33-04,. 9-A33-07. 01-Jul-2014. Rev. 2 to AFM. Supplement. A33 to AF
Garmin G1000,
DA 40 NG AFM
SBAS and P-RNAV
Supplement A33
Operation
SUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 40 NG Integrated Avionics System Garmin G1000, SBAS and P-RNAV Operation Doc. No.
:
6.01.15-E
Date of Issue
:
12-Jan-2011
Design Change Advisory
:
OÄM 40-336
This Supplement to the Airplane Flight Manual is EASA approved under Approval Number 10035550.
DIAMOND AIRCRAFT INDUSTRIES GMBH N.A. OTTO-STR. 5 A-2700 WIENER NEUSTADT AUSTRIA
9-A33-1
Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
Intentionally left blank.
Page 9-A33-2
12-Jan-2011
Rev. 0
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Garmin G1000,
DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
0.1
Rev. No.
RECORD OF REVISIONS
Reason
Chapters
Page(s)
9-A33-03, 1
Correction
0, 2
9-A33-04, 9-A33-10
9-A33-03, AFM 0, 1
2
9-A33-04,
Revision 3 9-A33-07
Doc. # 6.01.15-E
Date of Revision
Approval Note
Date of Approval
Date Inserted
Signature
Rev. 1 to AFM Supplement A33 to AFM Doc. No. 6.01.15-E is 23-Aug-2011 16-Aug-2011 approved under the authority of DOA No. EASA 21J.052 Rev. 2 to AFM Supplement A33 to AFM Doc. No. 6.01.15-E is 29-Jan-2015 01-Jul-2014 approved under the authority of DOA No. EASA 21J.052
01-Jul-2014
Rev. 2
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Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
0.2
LIST OF EFFECTIVE PAGES
Chapter
Page
Date 9-A33-1
12-Jan-2011
9-A33-2
12-Jan-2011
9-A33-3
01-Jul-2014
9-A33-4
01-Jul-2014
9-A33-5
12-Jan-2011
9-A33-6
12-Jan-2011
9-A33-7
01-Jul-2014
9-A33-8
12-Jan-2011
EASA approved 9-A33-9
12-Jan-2011
EASA approved 9-A33-10
16-Aug-2011
EASA approved 9-A33-11
12-Jan-2011
EASA approved 9-A33-12
12-Jan-2011
EASA approved 9-A33-13
12-Jan-2011
3
9-A33-14
12-Jan-2011
4A
9-A33-14
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4B
9-A33-14
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5, 6, 7, 8
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Doc. # 6.01.15-E
Garmin G1000,
DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
0.3
TABLE OF CONTENTS
1.
GENERAL .................................................................................................. 9-A33-6
2.
OPERATING LIMITATIONS ...................................................................... 9-A33-9
3.
EMERGENCY PROCEDURES ................................................................ 9-A33-14
4A.
NORMAL OPERATING PROCEDURES ............................................. 9-A33-14
4B.
ABNORMAL OPERATING PROCEDURES......................................... 9-A33-14
5.
PERFORMANCE ..................................................................................... 9-A33-14
6.
MASS AND BALANCE ............................................................................. 9-A33-14
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ...................... 9-A33-14
8.
AIRPLANE HANDLING, CARE AND MAINTENANCE ............................ 9-A33-14
Doc. # 6.01.15-E
12-Jan-2011
Rev. 0
Page 9-A33-5
Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
1.
GENERAL
1.5 DEFINITIONS AND ABBREVIATIONS (i) Miscellaneous AC:
Advisory Circular
AMC:
Acceptable Means of Compliance
AIRAC:
Aeronautical Information Regulation and Control
SBAS:
Satellite Based Augmentation System
WAAS:
Wide Area Augmentation System
EGNOS:
European Geostationary Navigation Overlay Service
MSAS:
Multi-functional Satellite Augmentation System
RNAV:
Area Navigation
P-RNAV:
Precision Area Navigation
B-RNAV:
Basic Area Navigation
LPV:
Localizer Performance with Vertical Guidance
LNAV/VNAV:
Lateral Navigation / Vertical Navigation
LNAV+V:
Lateral Navigation with Advisory Vertical Guidance
RNP:
Required Navigation Performance
GNSS:
Global Navigation Satellite System
STAR:
Standard Terminal Arrival Route
SID:
Standard Instrument Departure
ETSO:
European Technical Standard Order
RAIM:
Receiver Autonomous Integrity Monitoring
WFDE:
WAAS Fault Detection/Exclusion
Page 9-A33-6
12-Jan-2011
Rev. 0
Doc. # 6.01.15-E
Garmin G1000,
DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
1.8 1.9 G1000 AVIONICS SYSTEM The Garmin GNSS navigation system installed in this airplane is a GPS system with a Satellite Based Augmentation System (SBAS) comprised of two TSO-C145a Class 3 approved Garmin GIA 63Ws, TSO-C146a Class 3 approved Garmin GDU 104X Display Units, Garmin GA36 antennas, and GPS/WAAS software version 3.1 or later approved version. The Garmin GNSS navigation system in this airplane is installed in accordance with FAA AC 20-138B, EASA AMC 20-27 and EASA NPA 2009 (AMC 20-28).
NOTE The following listing of the Garmin G1000 operational capabilities does not constitute an operational approval. For the operational approval of the airplane contact the appropriate governing authority.
The Garmin GNSS navigation system as installed in this airplane complies with the requirements of FAA AC 20-138B, EASA AMC 20-27 and EASA AMC 20-28 and is approved for navigation using GPS and SBAS (within the coverage of a Satellite Based Augmentation System complying with ICAO Annex 10) for IFR enroute, terminal area, and non-precision approach operations (including those approaches titled “GPS” and “RNAV (GPS)” approaches). The Garmin GNSS navigation system installed in this airplane is approved for approach procedures with vertical guidance including “LPV”, “LNAV/VNAV” and LNAV+V, within the European and U.S. National Airspace System. The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements of FAA AC 90-105 and meets the equipment performance and functional requirements to conduct RNP terminal departure and arrival procedures and RNP approach procedures without RF (radius to fix) legs.
Doc. # 6.01.15-E
01-Jul-2014
Rev. 2
Page 9-A33-7
Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements of FAA AC 90-100A for RNAV 2 and RNAV 1 operations. The Garmin GNSS navigation system as installed in this airplane has been found to comply with the requirements for primary means of Class II navigation in oceanic and remote navigation (RNP-10) without time limitations in accordance with FAA AC 20-138B and FAA Order 8400.12A. The Garmin GNSS navigation system can be used without reliance on other long-range navigation systems. The Garmin GNSS navigation system as installed in this airplane has been found to comply with the navigation requirements for primary means of Class II navigation in oceanic and remote navigation (RNP-4) in accordance with FAA AC 20-138B and FAA Order 8400.33. The Garmin GNSS navigation system can be used without reliance on other long-range navigation systems. Additional equipment may be required to obtain operational approval to utilize RNP-4 performance. The Garmin GNSS navigation system as installed in this airplane complies with the accuracy, integrity, and continuity of function, and contains the minimum system
functions
required
for
PRNAV
operations
in
accordance
with
JAA Administrative & Guidance Material Section One: General Part 3: Temporary Guidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1). The GNSS navigation system has two ETSO-145 / TSO-C145a Class 3 approved Garmin GIA 63Ws, and ETSO-146 / TSO-C146a Class 3 approved Garmin GDU 104X Display Units. The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements for PRNAV and BRNAV operations in accordance with FAA AC 90-96A and JAA TGL-10 Rev 1 and AMC 20-4. Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with FAA AC 20-153 for database Integrity, quality, and database management practices for the Navigation database. Pilots and operators can view the LOA status at www.Garmin.com > Aviation Databases > Type 2 LOA Status. Navigation
Page 9-A33-8
information
is
referenced
12-Jan-2011
to
WGS-84
Rev. 0
reference
system.
Doc. # 6.01.15-E
Garmin G1000,
DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
2.
OPERATING LIMITATIONS
2.16 OTHER LIMITATIONS 2.16.9
G1000 GPS NAVIGATION SYSTEM LIMITATIONS
NOTE The following set of limitations supersedes the limitations addressing the same functions of the G1000 in the basic AFM limitation section. All other Garmin G1000 Avionic System limitations remain effective. The following placard is no longer applicable:
GPS NOT APPROVED FOR WAAS OPERATIONS
Flight Preparation Phase For flight planning purposes, operations on RNP and RNAV procedures when SBAS signals are not available, the availability of GPS integrity RAIM shall be confirmed for the intended route of flight. In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight, the flight should be delayed, cancelled, or re-routed on a track where RAIM requirements can be met. For flight planning purposes for operations within European B-RNAV and P-RNAV airspace, if more than one satellite is scheduled to be out of service, then the availability of GPS integrity RAIM shall be confirmed for the intended flight (route and time). In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended flight, the flight should be delayed, cancelled, or re-routed on a track where RAIM requirements can be met.
Doc. # 6.01.15-E
EASA approved
12-Jan-2011
Rev. 0
Page 9-A33-9
Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
For flight planning purposes, operations where the route requires Class II navigation the airplane’s operator or pilot-in-command must use the Garmin WFDE Prediction program to demonstrate that there are no outages on the specified route that would prevent the Garmin GNSS navigation system to provide primary means of Class II navigation in oceanic and remote areas of operation that requires (RNP-10 or RNP-4) capability. If the Garmin WFDE Prediction program indicates fault exclusion (FDE) unavailability will exceed 34 minutes in accordance with FAA Order 8400.12A for RNP-10 requirements, or 25 minutes in accordance with FAA Order 8400.33 for RNP-4 requirements, then the operation must be rescheduled when FDE is available.
NOTE Within the United States, RAIM availability can be determined using the Garmin WFDE Prediction program 3.00 or later approved version with Garmin GA36 antennas selected, or the FAA’s
enroute
and
terminal
RAIM
prediction
website:
www.raimprediction.net, or by contacting a Flight Service Station.
NOTE Within Europe, RAIM availability can be determined using the Garmin
WFDE
Prediction
program
or
Europe’s
AUGER GPS RAIM Prediction Tool at http://augur.ecacnav.com/ augur/app/home. For other areas, use the Garmin WFDE Prediction program. This requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of flight. The route planning and WFDE prediction program may be downloaded from the GARMIN website on the internet. For information on using the WFDE Prediction Program, refer to GARMIN
WAAS
FDE
Prediction
Program,
part
number
190-00643-01, ‘WFDE Prediction Program Instructions’. Navigation information is referenced to WGS-84 reference system, and should only be used where the Aeronautical Information Publication (including electronic data and aeronautical charts) conform to WGS-84 or equivalent. Page 9-A33-10
EASA approved
16-Aug-2011
Rev. 1
Doc. # 6.01.15-E
Garmin G1000,
DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation For flight planning purposes, it is not acceptable to plan a RNAV (GPS) LPV or LNAV/VNAV approach on the destination and alternate airport. The alternate airport must be planned using a LNAV approach or available ground-based aid.
Preflight Phase SBAS functionality must be enabled on the G1000 GPS Status page (refer to the G1000 Pilot’s Guide for procedure). The pilot must confirm at system initialization that the Navigation database is current. GPS/SBAS based IFR enroute, oceanic, and terminal navigation is prohibited unless the pilot verifies and uses a valid, compatible, and current Navigation database or verifies each waypoint for accuracy by reference to current approved data. Navigation database is expected to be current for the duration of the flight. If the AIRAC cycle will change during flight, the pilot must ensure the accuracy of navigation data, including suitability of navigation facilities used to define the routes and procedures for flight. If an amended chart affecting navigation data is published for the procedure, the database must not be used to conduct the procedure.
NOTE Discrepancies that invalidate a procedure must be reported to Garmin International. The affected procedure is prohibited from being flown using data from the Navigation database until a new Navigation database is installed in the airplane and verified that the discrepancy has been corrected. Contact information to report Navigation
database
discrepancies
can
be
found
at
www.Garmin.com > Support > Contact Garmin Support > Aviation. Pilots and operators can view navigation data base alerts at www.Garmin.com > In the Air > NavData Alerts.
Doc. # 6.01.15-E
EASA approved
12-Jan-2011
Rev. 0
Page 9-A33-11
Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
Both Garmin GPS navigation receivers must be operating and providing GPS navigation guidance to their PFD for operations requiring RNP-4 performance. North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace operations per FAA AC 91-49 and FAA AC 120-33 require both GPS/SBAS receivers to be operating and receiving usable signals except for routes requiring only one Long Range Navigation sensor. In Flight Phase Manual entry of waypoints using latitude/longitude or place/bearing is prohibited.
NOTE Whenever possible, RNP and RNAV routes including Standard Instrument
Departures
(SIDs)
and
Obstacle
Departure
Procedures (ODPs), Standard Terminal Arrival (STAR), and enroute RNAV “Q” and RNAV “T” routes should be loaded into the flight plan from the database in their entirety, rather than loading route waypoints from the database into the flight plan individually. Selecting and inserting individual named fixes from the database is permitted, provided all fixes along the published route to be flown are inserted. Approach Phase GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the Navigation database.
NOTE Not all published Instrument Approach Procedures (IAP) are in the Navigation database. Pilots planning on flying an RNAV instrument approach must ensure that the Navigation database contains the planned RNAV Instrument Approach Procedure and that approach procedure must be loaded from the Navigation database into the FMS flight plan by its name.
Page 9-A33-12
EASA approved
12-Jan-2011
Rev. 0
Doc. # 6.01.15-E
Garmin G1000,
DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
IFR non-precision approach approval using the GPS/SBAS sensor is limited to published approaches authorized by the appropriate governing authority. Advisory vertical guidance deviation information is only an aid to help pilots comply with altitude restrictions. When using advisory vertical guidance, the pilot must use the primary barometric altimeter to ensure compliance with all altitude restrictions, particularly during instrument approach operations. The navigation equipment required to join and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart. Use of the Garmin GPS/SBAS receivers to provide navigation guidance during the final approach segment of an ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for “or GPS” navigation is prohibited. When using the Garmin VOR/LOC/GS receivers to fly the final approach segment, VOR/LOC/GS navigation data must be selected and presented on the CDI of the pilot flying.
Doc. # 6.01.15-E
EASA approved
12-Jan-2011
Rev. 0
Page 9-A33-13
Garmin G1000, DA 40 NG AFM
SBAS and
Supplement A33
P-RNAV Operation
3.
EMERGENCY PROCEDURES No changes.
4A. NORMAL OPERATING PROCEDURES No changes.
4B. ABNORMAL OPERATING PROCEDURES No changes.
5.
PERFORMANCE No changes.
6.
MASS AND BALANCE No changes.
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS No changes.
8.
AIRPLANE HANDLING, CARE AND MAINTENANCE No changes.
Page 9-A33-14
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Rev. 0
Doc. # 6.01.15-E
